| Titre : | Applications of robust control to nonlinear systems | | Type de document : | texte imprimé | | Auteurs : | Richard Colgren, Auteur | | Editeur : | United States : American Institute of Aeronautics | | Année de publication : | 2004 | | Collection : | Progress in Astronautics and Aeronautics | | Importance : | 175 p. | | Présentation : | couv. ill. en coul., ill. | | Format : | 24 cm. | | ISBN/ISSN/EAN : | 978-1-563-47666-2 | | Langues : | Anglais (eng) | | Catégories : | AUTOMATISME
| | Index. décimale : | 25-07 Théorie de la commande: commandes des processus | | Résumé : | This book offers a three-step approach to generating a robust nonlinear controller: modeling, synthesis and robustness analysis. The publication is targeted to practicing engineers and graduate-level students working in guidance, information command and control systems, and CAD/CAM. The methods covered in this book allow the user to design and analyze nonlinear controllers for nonlinear systems with several important and unique characteristics: the ability to specify the closed loop system's frequency response via requirements on the sensitivity (S) and complementary sensitivity (T), the ability to directly minimize an undesirable resonance or peak in the frequency response while simultaneously closing all loops from the input to the output vector in essentially one single design step, and the ability to analyze the stability characteristics for multiple independent and dependent problem variables. | | Note de contenu : | Table of contents:
Chapter1 Introduction to robust control
Chapter2 The Describing Function
Chapter3 H Optimal Control
Chapter4 Robustness Analysis via Simplicial Algorithms
Chapter5 Nonlinear H Control
Chapter6 Direct Approaches to Nonlinear H Control
Chapter7 Nonlinear H Control of a UAV
Chapter8 Computer Algorithms
Chapter9 Hardware Implementations Example
Chapter10Pilotes Aircraft Performance |
Applications of robust control to nonlinear systems [texte imprimé] / Richard Colgren, Auteur . - United States : American Institute of Aeronautics, 2004 . - 175 p. : couv. ill. en coul., ill. ; 24 cm.. - ( Progress in Astronautics and Aeronautics) . ISBN : 978-1-563-47666-2 Langues : Anglais ( eng) | Catégories : | AUTOMATISME
| | Index. décimale : | 25-07 Théorie de la commande: commandes des processus | | Résumé : | This book offers a three-step approach to generating a robust nonlinear controller: modeling, synthesis and robustness analysis. The publication is targeted to practicing engineers and graduate-level students working in guidance, information command and control systems, and CAD/CAM. The methods covered in this book allow the user to design and analyze nonlinear controllers for nonlinear systems with several important and unique characteristics: the ability to specify the closed loop system's frequency response via requirements on the sensitivity (S) and complementary sensitivity (T), the ability to directly minimize an undesirable resonance or peak in the frequency response while simultaneously closing all loops from the input to the output vector in essentially one single design step, and the ability to analyze the stability characteristics for multiple independent and dependent problem variables. | | Note de contenu : | Table of contents:
Chapter1 Introduction to robust control
Chapter2 The Describing Function
Chapter3 H Optimal Control
Chapter4 Robustness Analysis via Simplicial Algorithms
Chapter5 Nonlinear H Control
Chapter6 Direct Approaches to Nonlinear H Control
Chapter7 Nonlinear H Control of a UAV
Chapter8 Computer Algorithms
Chapter9 Hardware Implementations Example
Chapter10Pilotes Aircraft Performance |
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